Allison AE-3007C
Service difficulty reports · 793
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE engine_model_key = 'AE3007C' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE engine_model_key = 'AE3007C' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 2010FA0000016Carbon Seal · wornOIL FOUND AT 6:00 POS INSIDE FAN CASE. NR O CARBON SEAL WAS REPLACED. REPLACED IAW MM 72-25-25.SDR 2009F00142Fadec · malfunctionedAFTER ADVANCING THROTTLES TO TAKEOFF POSITION AND APPROX 5 SECONDS INTO THE TAKEOFF ROLL SIMULTANEOUS AMBER FADEC REV ADC R AND FADEC REV ADC L CAS ILLUMINATES. RESET FADECS WITH MESSAGE RE-APPEARING ON 2ND ATTEMPT.SDR V0XR201001110004Floor Support · corrodedFLOOR PANEL PROFILE AT FRAME X 6523 OTBD OF RY .479 HAS CORROSION. REMOVED AND REPLACED PROFILE.SDR V0XR201001110005Floor Support · corrodedFLOORBOARD PROFILE AT STA X 5418 RY .479 HAS CORROSION. REMOVED AND REPLACED PROFILE.SDR V0XR201001110007Floor Support · corrodedFLOORBOARD PROFILE AND INBD SIDE OF FRAME AT LY 479 AT STA X 5833 HAS CORROSION. REMOVED AND REPLACED PROFILE.SDR V0XR201001110008Seat Track · corrodedOTBD SIDE OF SEATRAIL AT LY .479 FROM X.5418 - X.6523 HAS CORROSION. R & R DIGITAL.SDR V0XR201001110009Sill · corrodedLT FLOORBOARD PROFILE AT STA X 5633 OTBD OF LY .479 HAS CORROSION. R & R SILL.SDR V0XR201001110010Gusset · corrodedSUPPORT BEAM AROUND SOME NUTPLATES HAVE CORROSION. R & R GUSSET.SDR V0XR201001110011Frame · corrodedFRAME TOP PROFILE AT FRAME 62 LY .479 HAS CORROSION. R & R PROFILE.SDR V0XR201001110012Frame · corrodedFRAME TOP PROFILE AT FRAME 62 RY .479 - .644 HAS CORROSION. REMOVED AND REPLACED PROFILE. W/C 1088SDR V0XR201001110013Doubler · corrodedDOUBLER RT .479 FRAME 22 HAS CORROSION. R & R DOUBLER.SDR V0XR201001110014Doubler · corrodedDOUBLER AT RT .479 FRAME 20R HAS CORROSION. R & R DOUBLER.SDR V0XR201001110001Profile · corrodedFLOORBOARD PROFILES AT Y.0 AND LY .479 HAVE LIGHT PITTING AND CORROSION FROM STA X 7131 - X 14513. REMOVED AND REPLACED PROFILES.SDR V0XR201001110002Profile · corrodedOTBD FLOORBOARD PROFILES AT LY .479 HAVE LIGHT PITTING AND CORROSION FROM STA X 99641 - X 14823. REMOVED AND REPLACED PROFILES.SDR CA091128001Acm · odor(CAN) DURING GROUND OPERATION, FLIGHT CREW OBSERVED AN ODOR IN THE CABIN, FOLLOWED BY HOT AIR BEING CIRCULATED IN THE CABIN. OPERATING THE TEMPERATURE CONTROLS IT WAS NOTED THAT THE COCKPIT ACM DUCT SUPPLY TEMPERATURE WAS RISING, REGARDLESS OF CABIN TEMP SELECSDR DXTA2009111603861Fadec · malfunctionedAFTER TAKEOFF, AMBER "FAN DAMAGE R" CAS MESSAGE ILLUMINATED. THE RT ENGINE WAS STILL PRODUCING SUFFICENT THRUST AND NO VIBRATION WAS APPARENT. THE RT ENGINE THRUST MODE INDICATOR DISPLAYED "T/O" IN AMBER AND REMAINED ON AFTER ENGINE SHUTDOWN. DURING THE TAXI BSDR DXTA200911160386Fadec · inoperativeREMOVED AND REPLACED RT ENG FADEC B IAW MM, CH 76-12-00. OPS CHECK GOOD.SDR AWKA7561028Seal · leakingTHE FLIGHT CREW RECEIVED A RT ENG FIRE LIGHT AND ASSOCIATED EICAS MESSAGE ON TAKEOFF ROLL AT 75 KIAS. LIGHTS WENT OUT WHEN PWR WAS REDUCED TO IDLE. ENG FIRE EXTINGUISHING SYS WAS NOT ACTIVATED. THE ACFT WAS INSPECTED BY MX AND WORN HIGH PRESSURE BLEED AIR DSDR DJFA2009035Engine · bird ingestionON TAKE-OFF, CREW REPORTED BURNING ODOR IN THE CABIN. ACFT RETURNED TO THE DEPARTURE AIRPORT WITHOUT INCIDENT. AIRCRAFT HAD INGESTED A BIRD ON THE PREVIOUS LEG. MAINTENANCE INSPECTED THE ENGINE AGAIN AND CLEANED MINOR DEBRIS (BIRD REMENANTS) FROM THE BYPASSSDR SIMA20092401Engine · malfunctionedON FLIGHT 4773 THE CREW REPORTED AFTER THRUST LEVERS WERE PUT INTO NOTCH DURING TAKEOFF ROLL THE AIRCRAFT LURCHED TO THE LEFT. THE CREW ELECTED TO ABORT THE FLIGHT AND THEN SMELLED SMOKE. THE CREW SECURED THE ENGINE AND THE SMOKE SMELL WENT AWAY ON NR 1 ENGISDR DJFA2009034Engine · failedCREW REPORTED IN FLIGHT ENG FAILURE OF THE RT ENG ON CLIMB OUT. AT FL070 CREW ADVANCED THROTTLES FOR UNRESTRICTED CLIMB TO FL190. AT THAT MOMENT, THE RT ENG PRODUCED A LOUD BANG AND LOST PWR. NO ATTEMPTS WERE MADE TO RESTART ENG AND EMERGENCY HANDLING WAS RSDR SIMA200921103Engine · power lossON FLIGHT 3996 CREW REPORTED IN CRUISE ENGINE 2 ROLL BACK OCCURRED. AIRCRAFT RETURNED TO CHA. AIRCRAFT LANDED SAFELY. AIRCRAFT REMOVED FROM SERVICE. ISSUED MEL 78-1, PER FLIGHT DATA RECORDER, DATA READOUT TESTED ENGINE 2 THRUST REVERSER FADEC INTERFACE WIRSDR CA090219008Switch · failed(CAN) FLIGHT CREW REPORTED RT REVERSER FAILED TO DEPLOY ON LANDING. SYS TROUBLESHOT AND FAULT ISOLATED TO THE OTBD DEPLOY SWITCH. SWITCH REPLACED IAW KIT DS231-1-2SKS AND REVERSER FUNCTION TESTED SERVICEABLE IAW 78.SDR DXTA2009021703509Engine · making metalDURING TAKE OFF ROLL GOT "CHIP DETECT -R" AMBER CAS MESSAGE. ABORTED TAKEOFF. EXAMINED ALL RT ENG MAGNETIC PLUGS FOR PARTICLES. FOUND CHIP, REPLACED OIL FILTER AND COMPLIED WITH OIL FILTER AND ANALYZER KIT. OPERATED THE RT ENG, "CHIP DETECTER" CAS MESSAGE DIDSDR DJFA2009010Oil System · leakingIN FLIGHT, CREW REPORTED AN OIL ODOR AND SMOKE HAZE IN THE COCKPIT AND CABIN. ADDITIONALLY, THE CREW MONITORED THE OIL QTY FOR THE REMAINDER OF THE FLIGHT AND REPORTED LOOSING ABOUT 1 QUART OF OIL PER HOUR. THE ACFT DIVERTED AND LANDED SAFELY. MX ISOLATED THSDR DJFA2009009Carbon Seal · leakingDURING FLIGHT CREW REPORTED AN OILY BURNING ODOR FROM THE AIR CONDITIONING DUCTS. CREW DEACTIVATED THE FWD AC PAC AND THE ODOR WENT AWAY. MX FOUND THE NR1 ENGINE ACCY GEARBOX BREATHER ADAPTOR CARBON SEAL LEAKING. THE SEAL WAS REPLACED AND THE LEAK WAS STILL SDR DXTA2009012803476Warning Light · false activationFUEL FILTER BYPASS LT AMBER CAS MSG IN FLIGHT. INSP THE LT ENG FUEL FILTER. NO DEFECTS NOTED. REINSTALLED SAME. NO FILTER BYPASS CAS MESSAGE WAS FOUND ON INSP. PERFORMED FUNCTIONAL TEST OF FUEL FILTER PYPASS INDICATING SYS IAW MM CH 73-37-10. OPS CHECKS SDR DXTA2009012203470Warning Light · illuminatedFUEL FILTER BYPASS L CAS MESSAGE ILLUMINATED IN FLIGHT.SDR DXTA2009012103470Connector · looseFUEL FILTER BYPASS L CAS MESSAGE ILLUMINATED IN FLIGHT. MESSAGE ONLY STAYED ON APPROX 1 MINUTE, SECOND EACH OCCURENCE, BUT WOULD REAPPEAR EVERY FEW MINUTES. THIS CONTINUED LANDING. FOUND FUEL FILTER BYPASS SWITCH ELECTRICAL CONNECTOR TO BE LOOSE AND DIRTY. SDR CA081201006Dome Nut · corroded(CAN) DURING THE REPLACEMENT OF THE RT WINDSHIELD, DUE TO A BROKEN OUTER PANE, HEAVY CORROSION WAS NOTED COMING OUT OF THE DOME NUTS. THE WINDSHIELD IS INSTALLED FROM THE OUTSIDE AND THE SCREWS ARE HELD IN PLACE BY THESE DOME NUTS THAT RIVETED IN PLACE AROUND SDR CA081126005Antenna · malfunctioned(CAN) FLIGHT CREW REPORTED NR 2 FMS DRIFTED 8NM AT END OF THE LEG. NR 2 GPS ANTENNA REPLACED AND TESTED SERVICEABLE IAW 34-54-01.SDR CA081126007Display · failed(CAN) RE-OCCURRING DEFECT 2008/10/21 -FLIGHT CREW REPORTED NR 4 DISPLAY UNIT FLICKED ON START-UP. FAULT COULD NOT BE DUPLICATED AND WAS SWAPPED TO NR4 POSITION FOR TROUBLESHOOTING PURPOSES. 2008/10/22 -FLIGHT CREW REPORTED NR3 DISPLAY UNIT FAILED AT THE TOP OSDR 2008FA0000772Controller · failedFLAPS HARD FAILED DURING FLIGHT. FOUND THAT THE FLAP CONTROLLER HARD FAILED DURING COLD SOAKING. REPLACED FLAP CONTROLLER AND ACCOMPLISHED SATISFACTORY FLAP FUNCTIONAL CHECK WITH NO DEFECTS NOTED. RETURNED ACFT TO SERVICE. (K)SDR RAIA00809023Bleed Valve · malfunctionedENG 2 ITT RISE ABOVE 900 IN AMBER WHILE THRUST LEVER IN DETENT. MAINT REMOVED AND REPLACED THE NR 2 ENG COMPRESSOR ACCELERATION BLEED CONTROL VALVE. ENG RUN OPS CHECKED GOOD. (K)SDR DXT2008F00000Unknown · smokeAFTER INITIAL START OF APU UPON OPENING BLEED AIR AND ISOLATION VALVE, LT LOWER COCKPIT AREA BEGAN FILLING WITH BLUE/GREY SMOKE AND UPON SHUTDOWN OF APU AND CLOSING ISOL VALVE/BLEED VALVE, SMOKE DISSIPATED. (K)SDR FDK2008F00005Battery · dischargedGALLEY EMERGENCY LIGHT INOP. MX REPLACED NR 2 EMERGENCY LIGHT BATTERY PACK ASSY, OPS CHECK GOOD. (K)SDR DXTA200803082Bolt · missingGEAR UNLOCK LIGHT REMAINED ON AFTER GEAR RETRACTION. FOUND RT MLG TRAILING LINK THROUGH BOLT MISSING.SDR DJFA2008046Acm · seizedWITH APU ONLY, OPERATING, SMOKE ENTERED COCKPIT/CABIN WEMAC VENTS HOT TO TOUCH. MAINT TROUBLESHOT SYS TO SEIZED AIR CYCLE MACHINE (FORWARD). REMOVED ACM, INSTALLED REPAIRED ACM, AND NEW COALESCER SOCK.SDR DXTA200803076Actuator · inoperativeDURING CLIMBOUT THROUGH APPROX 7000 FT AGL IN GUSTY WINDS A RUD LIMIT FAIL A ILLUMINATED WITH RUDDER LIMIT AT 27 PERCENT .SDR DXTA200803077Warning System · activated"FGC- B FAIL" CAS MESSAGE CAME ON 45 MIN INTO FLIGHT. DID NOT RESET.SDR DXTA200803075Bulb · intermittentON FINAL LT MLG DOWN INDICATOR LIGHT DID NOT ILLUMINATE. REMOVED INTERMITTENT LT MLG DOWNLOCK. INDICATOR BULBS & INSTALLED NEW BULBS IAW MM 32-60-00. OPERATED NORMAL NO DEFECTS.SDR DXTA200803067Connector · looseGEAR BUMP HEARD AND FELT 3 TIMES DURING CLIMB. FOUND RT MLG DOOR LOOSE & RT UPLOCK SWITCH CONNECTOR LOOSE. TIGHTENED RT UPLOCK SWITCH CONNECTOR & ADJUSTED RT MLG DOOR. OPERATIONAL CHECKS GOOD ON GEAR SWING, ALSO, ACCOMPLISHED GEAR BUMP TROUBLESHOOTING IAW MMSDR DXTA200803066Computer · false activationAT CRUISE ALTITUDE FL410 A PULSATING THUMP COULD BE FELT IN BOTH CONTROL COLUMNS. INSPECTED, ALL PANELS, FLT CONTROLS DOORS ETC. NO DEFECTS NOTED. REMOVED AND REPLACED RT AOA COMPUTER IAW MM 34-14-01 C/W FT OF AOA SYSTEM PER SAME OPS CHECK GOOD.SDR DJFA2008045Acm · seizedPILOT REPORTED: DURING TAXI THE CABIN FILLED WITH SMOKE; MX INSPECTED ACM'S AND NOTED THE CABIN ACM WAS SEIZED. THE CABIN ACM WAS REMOVED AND REPLACED.SDR DXTA200803057Feel Sensor · bindingIN FLIGHT, AILERON FLIGHT CONTROLS ARE BINDING WHILE TURNING BOTH LT AND RT. REMOVED AND REPLACED ARTIFICIAL FEEL BUNGEE. PERFORMED OPS CHECKS AND ADJUSTMENTS ALL OK.SDR DXTA200803058Actuator · inoperativeDURING CLIMB AND CRUISE, RUDDER OSCILLATES INTERMITTENTLY WITH UPPER RUDDER (A) SELECTED. REMOVED UPPER RUDDER ACTUATOR- INSTALLED A REPAIRED ACTUATOR. PERFORMED OPERATIONAL AND LEAK CHECK WITH SATISFACTORY RESULT. TRAVEL CHECKS NORMAL, MAINTENANCE PERFORMED SDR DXTA200803055Brake Assy · leakingRT BRAKE GRABS WITH MINIMAL PRESSURE APPLIED TO BRAKE PEDAL AND JERKS AIRPLANE IN SAME DIRECTION. REMOVED AND REPLACED NR 3 MAIN BRAKE ASSY. IAW MM 32-42-01 AND BRAKE BEEDING IAW MM 32-42-00 OPS CHECK LEAK CHECKS GOOD.SDR DXTA200803051Pitot Head · failedCLIMBING THROUGHT 10,000 FT, WE HAD A DUAL FGC FAILURE. INSPECTED LT AND RT PITOT PROBES. FOUND RT FWD DRAIN TO BE BLOCKED. THE RT AFT DRAIN, AND BOTH LT DRAINS HAVE DEBRIS INSIDE. REMOVED FAILED LT AND RT PITOT PROBES. INSTALLED NEW LT AND RT PITOT PROBES, PSDR DXTA200803050Unknown · odorON POST FLIGHT, FOUND CABIN TO HAVE FOUL ROTTEN SEAFOOD ODOR. FOUND SPILL UNDER LEXAN COVER ON BAR, CLEANED SPILL SMELLS GOOD. IAW M/M 20-32-00.SDR C2XA08RI060Potentiometer · defectiveFLIGHT 2678 - FLIGHT CREW REPORTED AIRCRAFT PULLS TO THE RT AT TAKEOFF AT 80 KNOTS. MX REMOVED AND REPLACED FEEDBACK POTENTIOMETER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.
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